Global Patent Index - EP 2374997 A2

EP 2374997 A2 20111012 - Component for a gas turbine engine

Title (en)

Component for a gas turbine engine

Title (de)

Komponent für eine Gasturbine

Title (fr)

Composant pour un moteur à turbine à gaz

Publication

EP 2374997 A2 20111012 (EN)

Application

EP 11161120 A 20110405

Priority

US 75470410 A 20100406

Abstract (en)

A component (32) within a gas turbine engine includes a dead ended rib (56) which at least partially defines an internal cooling circuit flow path (26), the dead ended rib defines a bulbed rib profile (58).

IPC 8 full level

F01D 5/18 (2006.01)

CPC (source: EP US)

F01D 5/187 (2013.01 - EP US); F05D 2250/185 (2013.01 - EP US)

Designated contracting state (EPC)

AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR

Designated extension state (EPC)

BA ME

DOCDB simple family (publication)

EP 2374997 A2 20111012; EP 2374997 A3 20150218; EP 2374997 B1 20180606; US 2011243717 A1 20111006; US 8562286 B2 20131022

DOCDB simple family (application)

EP 11161120 A 20110405; US 75470410 A 20100406